US20060005730A1 - Rifled slug - Google Patents

Rifled slug Download PDF

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Publication number
US20060005730A1
US20060005730A1 US10/528,088 US52808805A US2006005730A1 US 20060005730 A1 US20060005730 A1 US 20060005730A1 US 52808805 A US52808805 A US 52808805A US 2006005730 A1 US2006005730 A1 US 2006005730A1
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United States
Prior art keywords
anterior
gun
central part
barrel
hollow space
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Granted
Application number
US10/528,088
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US7331294B2 (en
Inventor
Peter Mank
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Brenneke Wilhelm GmbH and Co KG
Original Assignee
Brenneke Wilhelm GmbH and Co KG
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Assigned to WILHELM BRENNEKE GMBH & CO. KG reassignment WILHELM BRENNEKE GMBH & CO. KG ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: MANK, PETER DR.
Publication of US20060005730A1 publication Critical patent/US20060005730A1/en
Application granted granted Critical
Publication of US7331294B2 publication Critical patent/US7331294B2/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B7/00Shotgun ammunition
    • F42B7/02Cartridges, i.e. cases with propellant charge and missile
    • F42B7/10Ball or slug shotgun cartridges

Definitions

  • the invention relates to a gun-barrel projectile having the characteristics of the preamble of claim 1 .
  • a predetermined breaking point is arranged between the rod-like central part and the piston-like bottom part of the end part, said breaking point being obtained at the time of manufacture in an injection molding process by insertion of a metal sleeve into the mold.
  • This manufacturing process is relatively costly and prolongs the cycle time at the time of manufacture.
  • a further drawback is the fact that the predetermined breaking point cannot be configured very uniformly. This has negative effects on the internal and external ballistics of the projectile.
  • the object of the present invention is to improve upon generic gun-barrel projectile, in that precision is increased; that is, the target spread is reduced.
  • the predetermined breaking point In the rear part of the gun-barrel projectile according to the invention, therefore, there is the predetermined breaking point between the hollow upper part and the rod-shaped central part. It can be manufactured at this position substantially more precisely and more cost-effectively than at the position according to the prior art and discussed hereinbefore.
  • a rending results upon lower gas pressure variations due to the lower tolerances of the predetermined breaking point; in other words, the gas pressure range in which the predetermined breaking point rends is smaller than in the prior art gun-barrel projectile. This has direct positive ramifications on the target accuracy.
  • a further advantage of the gun-barrel projectile according to the invention is in the fact that the posterior end of the rear part is formed in the flight phase by the formally precisely defined piston-shaped rear part. This results in defined flow relations, which positively influence the external ballistics of the projectile.
  • FIG. 1 represents a side view of a gun-barrel projectile before firing
  • FIG. 2 represents an illustration of the gun-barrel projectile according to FIG. 1 after firing
  • FIG. 3 represents a perspective representation of the rear part of the gun-barrel projectile before firing
  • FIG. 4 represents a side view of the rear part corresponding to FIG. 3 ;
  • FIG. 5 represents a section A-A according to FIG. 4 .
  • FIG. 6 represents an illustration of FIG. 5 after firing.
  • FIG. 1 represents a gun-barrel projectile, which is loaded in this form or in this condition by the manufacturer. It comprises a heavy lead head ( 1 ) and a lighter rear part ( 2 ) made out of lighter plastic. Because of the mass distribution, the gun-barrel projectile after leaving the gun barrel stabilizes in flight according to the arrow principle, because the center of gravity lies in front of the air attack point.
  • the lead head 1 has an essentially cylindrical shape and on its front surface it has a tip 3 , which is intended for improving the air resistance.
  • Slanted guide ribs 4 are distributed uniformly on the periphery. These guide ribs 4 enable passage through the choke of a gun, because they are urged away because of the ductility of the alloyed lead upon passing the choke. The load of the choke is, therefore, is no greater than in lead shot upon firing from the gun-barrel projectile.
  • the rear part 2 whose embodiment is best seen in FIG. 3-5 , is made of plastic in one piece using an injection molding technique. It consists of a anterior part 5 , a central part 6 and a posterior part 7 .
  • the anterior part 5 has a hollow cylindrical body 8 , which continues into a flange 9 of greater diameter towards the central part 6 .
  • the hollow cylindrical body 8 is seated with a slightly greater dimension in a corresponding cylindrical chamber in the lead head 1 , which is not apparent from the diagrammatic representation.
  • the flange 9 of the anterior part 5 serves as the support for the rear surface of the lead head 1 . In this fashion, upon firing, in co-operation with the hollow cylindrical body 8 an even distribution of the gas pressure is produced on the lead head 1 .
  • the anterior part 5 is provided with four air channels 12 , which are arranged evenly on the periphery.
  • these air channels 12 create a communication between the inside space of the hollow cylindrical body 8 and the atmosphere. They extend through the anterior face of the hollow cylindrical body 8 , which abut in the assembled condition on the bottom of the chamber in the lead head 1 , and then run one the outside of the hollow cylindrical body 8 over the flange 9 outwards.
  • a flange 13 is provided in the interior walls of the hollow cylindrical body 8 by means of a increase in diameter. The function of the air channels 12 and of the flange 13 is explained in more detail in the following.
  • the central part 6 connects with the anterior part 5 via an annular predetermined breaking point 14 . It is cylindrical and executed as a hollow body.
  • the predetermined breaking point 14 can be produced at this point using an injection molding method relatively easily and with little variation in tolerance.
  • peripherally distributed barbed segments 15 are formed at the transition between the central part 6 and the anterior part 5 , which—as will be explained in the following—co-operate with the flange 13 of the anterior part.
  • the central part 6 transitions—as can be seen particularly in FIGS. 5 and 6 —relatively thickly walled into the posterior part 7 , so that at this transition point no break or no deformation can from at the time of firing.
  • the posterior part 7 is configured as an rearwardly open hollow cylinder, if a central plug 16 is eliminated.
  • the posterior part 7 has the approximate diameter of the flange 9 of the anterior part 5 and terminates at the posterior end with a peripheral seal lip 17 , which serves at the time of firing to seal the gas pressure to the barrel.
  • reinforcing ribs 18 distributed over its periphery.
  • FIG. 1 represents the loaded condition of the gun-barrel projectile.
  • a gas pressure builds, which acts on the cross-sectional area of the posterior part 7 . Due to this pressure build-up, the predetermined breaking point 14 rends and the central part 6 pushes—because of the inertia of the heavy lead head 1 —into the interior of the hollow cylindrical body 8 of the anterior part 5 . That happens abruptly.
  • the air forced out of the inside space of the hollow cylindrical body 8 can flow off easily via the air channels 12 , so that the incursion of the central part 6 into the anterior part 5 does not encounter any resistance due to pressure accumulation.
  • the gun-barrel projectile has thus assumed the form represented in FIG. 2 , with which it leaves the barrel of the weapon. This form is maintained until striking the target, because the central part 6 and the posterior part 7 are captively connected to the anterior part 5 .
  • This connection is realized by the co-operation of the barbed sections 15 of the central part 6 and the flange 13 in the inside walls of the hollow cylindrical body 8 .
  • the barb-shaped sections 15 lock behind the flange 13 , so that the central part 6 can not separate, at least not by the forces acting on the rear part 2 during the flight of the gun-barrel projectile.
  • the engagement between the anterior part and the central part 6 and posterior part 7 is sown in FIG. 6 .

Abstract

The invention relates to a rifled slug provided with a metal head (1) and a plastic rear part (2), which is made as a single piece from a pin-shaped front part (5), with a rod-shaped middle part (6) joined to the rear of said front part, and with a plunger-shaped rear part (7). The front part (5) is inserted from the rear into a pocket hole of the metal head (1) and is joined thereto in a captive manner. The aim of the invention is to improve a rifled slug of the aforementioned type whereby increasing the precision, i.e reducing the dispersion in the target. To this end, the front part (5) is provided in the form of a hollow body and is joined to the middle part (6) via a predetermined breaking point (14), whereby when shooting, the middle part (6) slides into the cavity of the front part (5) until the upper surface (19) of the rear part (7) strikes the lower surface (20) of the front part (5).

Description

  • The invention relates to a gun-barrel projectile having the characteristics of the preamble of claim 1.
  • This type of gun-barrel projectile is described in EP 0 341 543 B1. The upper part of the end part of this projectile is formed as a solid body. It has a slight radial expansion vis-à-vis the blind hole of in the lead head, so that it has to be inserted into it using a force. Then, at a plurality of locations on the periphery of the lead head, preferably at three places distributed uniformly on the periphery of the lead head, lead is driven pointwise radially inwardly, where the displaced lead flows into a peripheral groove of the upper part of the end part. This inward displacement of lead occurs using rod-shaped steel pins similar to a punched-in part. In virtue of the force fit of the upper part of the end part in the lead head and the pointwise incorporation of the lead in the upper part of the end part, the latter can be joined captively with the lead head.
  • In the case of this prior art gun-barrel projectile a predetermined breaking point is arranged between the rod-like central part and the piston-like bottom part of the end part, said breaking point being obtained at the time of manufacture in an injection molding process by insertion of a metal sleeve into the mold. This manufacturing process is relatively costly and prolongs the cycle time at the time of manufacture. A further drawback is the fact that the predetermined breaking point cannot be configured very uniformly. This has negative effects on the internal and external ballistics of the projectile.
  • In the evolution of firing the piston-like end part shifts upwards on the rod-like central part after detachment of the predetermined breaking point, until its upper side contacts the underside of the upper part. A barblike projection encircling the rod-like central part holds the end part on the central part thus preventing the central part from detaching itself rearwardly from the rod-like central during the flight phase of the projectile. During the flight phase the rear end of the rod-like central part projects rearwardly from the piston-like end part. This is a drawback for the external ballistics of the projectile, because of the flow conditions resulting therefrom in the posterior zone of the rear part. Also disadvantageous in this respect is the fact that the rearwardly projecting end of the rod-shaped central part is non-uniform in its external form because of the manufacturing process described.
  • In the hereinbefore described gun-barrel projectile a very good damping of the gas pressure increase is noted in the barrel. Nevertheless the predetermined breaking point rends after firing because of the relatively large tolerances from cartridge to cartridge caused by the manufacturing process at relatively widely differing gas pressures. This has effects on the further pressure development in the barrel and consequently on the exit velocity of the projectile. Accordingly, it leaves the barrel from firing to firing with relatively widely varying velocity, whereby target precision suffers.
  • The object of the present invention is to improve upon generic gun-barrel projectile, in that precision is increased; that is, the target spread is reduced.
  • This object is achieved according to the invention by the gun-barrel projectile having the characteristics of claim 1.
  • In the rear part of the gun-barrel projectile according to the invention, therefore, there is the predetermined breaking point between the hollow upper part and the rod-shaped central part. It can be manufactured at this position substantially more precisely and more cost-effectively than at the position according to the prior art and discussed hereinbefore. A rending results upon lower gas pressure variations due to the lower tolerances of the predetermined breaking point; in other words, the gas pressure range in which the predetermined breaking point rends is smaller than in the prior art gun-barrel projectile. This has direct positive ramifications on the target accuracy.
  • A further advantage of the gun-barrel projectile according to the invention is in the fact that the posterior end of the rear part is formed in the flight phase by the formally precisely defined piston-shaped rear part. This results in defined flow relations, which positively influence the external ballistics of the projectile.
  • Other advantageous embodiments of the gun-barrel projectile are disclosed in the subordinate clams. The invention will be explained more completely in the following using an exemplary embodiment. In the relevant drawings:
  • FIG. 1 represents a side view of a gun-barrel projectile before firing;
  • FIG. 2 represents an illustration of the gun-barrel projectile according to FIG. 1 after firing;
  • FIG. 3 represents a perspective representation of the rear part of the gun-barrel projectile before firing;
  • FIG. 4 represents a side view of the rear part corresponding to FIG. 3;
  • FIG. 5 represents a section A-A according to FIG. 4, and
  • FIG. 6 represents an illustration of FIG. 5 after firing.
  • FIG. 1 represents a gun-barrel projectile, which is loaded in this form or in this condition by the manufacturer. It comprises a heavy lead head (1) and a lighter rear part (2) made out of lighter plastic. Because of the mass distribution, the gun-barrel projectile after leaving the gun barrel stabilizes in flight according to the arrow principle, because the center of gravity lies in front of the air attack point.
  • The lead head 1 has an essentially cylindrical shape and on its front surface it has a tip 3, which is intended for improving the air resistance. Slanted guide ribs 4 are distributed uniformly on the periphery. These guide ribs 4 enable passage through the choke of a gun, because they are urged away because of the ductility of the alloyed lead upon passing the choke. The load of the choke is, therefore, is no greater than in lead shot upon firing from the gun-barrel projectile.
  • The rear part 2, whose embodiment is best seen in FIG. 3-5, is made of plastic in one piece using an injection molding technique. It consists of a anterior part 5, a central part 6 and a posterior part 7. The anterior part 5 has a hollow cylindrical body 8, which continues into a flange 9 of greater diameter towards the central part 6. In the assembled gun-barrel projectile (FIG. 1) the hollow cylindrical body 8 is seated with a slightly greater dimension in a corresponding cylindrical chamber in the lead head 1, which is not apparent from the diagrammatic representation. Along with the force fit between this chamber in the lead head 1 and the hollow cylindrical body 8 the captive connection of the lead head 1 and the rear part 2 is obtained, in that the lead is pressed by means of a needle-like stamp in the fashion of a punched-in part into a peripheral groove 10 of the hollow cylindrical body 8. This type of punched-in part 11 can be seen in the diagrammatic representation according to FIGS. 1 and 2. In general, the connection is made by means of two or three punched-in parts 11 evenly distributed on the periphery.
  • The flange 9 of the anterior part 5 serves as the support for the rear surface of the lead head 1. In this fashion, upon firing, in co-operation with the hollow cylindrical body 8 an even distribution of the gas pressure is produced on the lead head 1.
  • The anterior part 5 is provided with four air channels 12, which are arranged evenly on the periphery. When the lead head 1 is in place, these air channels 12 create a communication between the inside space of the hollow cylindrical body 8 and the atmosphere. They extend through the anterior face of the hollow cylindrical body 8, which abut in the assembled condition on the bottom of the chamber in the lead head 1, and then run one the outside of the hollow cylindrical body 8 over the flange 9 outwards. In addition, in the interior walls of the hollow cylindrical body 8 a flange 13 is provided by means of a increase in diameter. The function of the air channels 12 and of the flange 13 is explained in more detail in the following.
  • The central part 6 connects with the anterior part 5 via an annular predetermined breaking point 14. It is cylindrical and executed as a hollow body. The predetermined breaking point 14 can be produced at this point using an injection molding method relatively easily and with little variation in tolerance. On the outside surface, peripherally distributed barbed segments 15 are formed at the transition between the central part 6 and the anterior part 5, which—as will be explained in the following—co-operate with the flange 13 of the anterior part.
  • The central part 6 transitions—as can be seen particularly in FIGS. 5 and 6—relatively thickly walled into the posterior part 7, so that at this transition point no break or no deformation can from at the time of firing. The posterior part 7 is configured as an rearwardly open hollow cylinder, if a central plug 16 is eliminated. The posterior part 7 has the approximate diameter of the flange 9 of the anterior part 5 and terminates at the posterior end with a peripheral seal lip 17, which serves at the time of firing to seal the gas pressure to the barrel. For stabilizing the walls of the posterior part 7, same is provided with reinforcing ribs 18 distributed over its periphery.
  • In the following, the co-operation of the lead head 1 and the rear part 2 at the time of firing is described.
  • As has already been explained hereinbefore, FIG. 1 represents the loaded condition of the gun-barrel projectile. After firing of the propellant charge, a gas pressure builds, which acts on the cross-sectional area of the posterior part 7. Due to this pressure build-up, the predetermined breaking point 14 rends and the central part 6 pushes—because of the inertia of the heavy lead head 1—into the interior of the hollow cylindrical body 8 of the anterior part 5. That happens abruptly. When this happens, the air forced out of the inside space of the hollow cylindrical body 8 can flow off easily via the air channels 12, so that the incursion of the central part 6 into the anterior part 5 does not encounter any resistance due to pressure accumulation. At the end of this movement of the now two-part rear part 2, the upper surface 19 of the posterior part 7 contacts the lower surface 20 of the anterior part 5. The gun-barrel projectile has thus assumed the form represented in FIG. 2, with which it leaves the barrel of the weapon. This form is maintained until striking the target, because the central part 6 and the posterior part 7 are captively connected to the anterior part 5. This connection is realized by the co-operation of the barbed sections 15 of the central part 6 and the flange 13 in the inside walls of the hollow cylindrical body 8. After maximum depth penetration of the central part 6 into the anterior part 5, the barb-shaped sections 15 lock behind the flange 13, so that the central part 6 can not separate, at least not by the forces acting on the rear part 2 during the flight of the gun-barrel projectile. The engagement between the anterior part and the central part 6 and posterior part 7 is sown in FIG. 6.

Claims (4)

1. A gun-barrel projectile having a metal head and a rear part made of plastic, which is manufactured in one piece from a pin-shaped anterior part, a rod-shaped central part connecting rearwardly therewith and a piston-like posterior part, wherein the anterior part inserts rearwardly into a blind hole of the metal head and is captively connected therewith, characterized in that the anterior part (5) is executed as a hollow body and is connected with the central part (6) via a predetermined breaking point 14), whereby at the time of firing the central part (6) pushes into the hollow space of the anterior part (5) to such an extent, that the upper surface (19) of the posterior part (7) contacts the lower surface (20) of the anterior part.
2. The gun-barrel projectile according to claim 1, wherein the anterior part (5) is provided with air channels (12), which make possible flow of the air forced into the hollow space of the anterior part (5) upon penetration of the central part (6).
3. The gun-barrel projectile according to claim 1, wherein barb-shaped sections (15) are provided on the central part (6), which upon penetration of the central part (6) into the hollow space of the anterior body (5) grab behind a flange (13) in the watts of the hollow space of the anterior part (5).
4. The gun-barrel projectile according to claim 2, wherein barb-shaped sections (15) are provided on the central part (6), which upon penetration of the central part (6) into the hollow space of the anterior body (5) grab behind a flange (13) in the walls of the hollow space of the anterior part (5).
US10/528,088 2002-09-25 2003-09-04 Rifled slug Expired - Lifetime US7331294B2 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE10244571A DE10244571C1 (en) 2002-09-25 2002-09-25 Shotgun or smooth bore projectile, has hollow front section connected by location of intentional breakage to rear section which slides into it during firing
DE10244571.0 2002-09-25
PCT/DE2003/002934 WO2004029539A1 (en) 2002-09-25 2003-09-04 Rifled slug

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US20060005730A1 true US20060005730A1 (en) 2006-01-12
US7331294B2 US7331294B2 (en) 2008-02-19

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US10/528,088 Expired - Lifetime US7331294B2 (en) 2002-09-25 2003-09-04 Rifled slug

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US (1) US7331294B2 (en)
EP (1) EP1543288B1 (en)
AT (1) ATE326680T1 (en)
AU (1) AU2003266195A1 (en)
DE (2) DE10244571C1 (en)
ES (1) ES2264033T3 (en)
WO (1) WO2004029539A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070227391A1 (en) * 2005-01-26 2007-10-04 De Aguiar Carlos F Q Non-lethal ammunition projectile
USD852922S1 (en) 2017-09-14 2019-07-02 F. Richard Langner Slug for launching from a disruptor
USD853519S1 (en) 2017-09-14 2019-07-09 F. Richard Langner Piston for driving water out a disrupter

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7735422B2 (en) 2003-10-11 2010-06-15 Ruag Ammotec Gmbh Shotgun-barrel projectile with intercalation and cartridge
AT502547B1 (en) * 2005-10-13 2009-10-15 Winter Udo Mag CARTRIDGE
WO2008142457A2 (en) * 2007-05-18 2008-11-27 Kukhaleishvili, Rati Abramyan's method for imparting a rotary motion to a bullet in a firearm barrel channel and a bullet for a smooth-bore hunting arm
US9488455B1 (en) 2015-01-22 2016-11-08 Consolidated Nuclear Security, LLC Sabot assembly
USD866701S1 (en) 2018-01-18 2019-11-12 Brenneke Ammunition GmbH Bullet

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US3256816A (en) * 1964-09-10 1966-06-21 Ii James O Pilcher Extending boom for sounding rockets
US3677179A (en) * 1966-09-29 1972-07-18 Lester A Potteiger Telescoping ordnance device
US3842741A (en) * 1973-06-07 1974-10-22 Us Army Subprojectile launched from telescopic tubes
US4233902A (en) * 1978-11-24 1980-11-18 The United States Of America As Represented By The Secretary Of The Navy 76MM Rammable practice cartridge
US4624187A (en) * 1983-04-23 1986-11-25 Rheinmetall Gmbh Penetrator projectiles
US4964341A (en) * 1989-08-21 1990-10-23 Aai Corporation Projectile with ram air-extendible probe and ram air-extendible probe assembly therefor
US4977834A (en) * 1988-02-29 1990-12-18 Denis Jean Pierre Firearms ammunition, particularly game-shooting ammunition
US5164538A (en) * 1986-02-18 1992-11-17 Twenty-First Century Research Institute Projectile having plural rotatable sections with aerodynamic air foil surfaces
US5677505A (en) * 1990-03-22 1997-10-14 Dittrich; William A. Reduced energy cartridge
US6415718B1 (en) * 1999-08-27 2002-07-09 Lambeth Properties Limited Training cartridge for a self loading gun
US6422149B1 (en) * 1999-08-27 2002-07-23 Lambath Properties Limited Blank training cartridge for a self loading gun
US6492632B1 (en) * 1999-01-28 2002-12-10 Irvin Pollin Lock and slide mechanism for tube launched projectiles
US6502516B1 (en) * 2000-01-18 2003-01-07 Anthony E. Kinchin Sabot shotgun slug assembly
US6679178B2 (en) * 2000-12-21 2004-01-20 Gueorgui M. Mihaylov Smooth bore barrel system with self spinning ammunition

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BE866822A (en) * 1978-05-09 1978-11-09 Herstal Sa BALL FOR SMOOTH BARREL SHOTGUNS
DE3815738A1 (en) * 1988-05-07 1989-11-16 Brenneke Wilhelm Kg CARTRIDGE WITH RIFLE RIFLE BULLET
DE4137315A1 (en) * 1991-11-13 1993-05-19 Brenneke Wilhelm Kg Cartridge for shotgun with rifled barrel - has round lead noise connected by shallow part-conical section to cylindrical section with sloping grooves on surface

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3256816A (en) * 1964-09-10 1966-06-21 Ii James O Pilcher Extending boom for sounding rockets
US3677179A (en) * 1966-09-29 1972-07-18 Lester A Potteiger Telescoping ordnance device
US3842741A (en) * 1973-06-07 1974-10-22 Us Army Subprojectile launched from telescopic tubes
US4233902A (en) * 1978-11-24 1980-11-18 The United States Of America As Represented By The Secretary Of The Navy 76MM Rammable practice cartridge
US4624187A (en) * 1983-04-23 1986-11-25 Rheinmetall Gmbh Penetrator projectiles
US5164538A (en) * 1986-02-18 1992-11-17 Twenty-First Century Research Institute Projectile having plural rotatable sections with aerodynamic air foil surfaces
US4977834A (en) * 1988-02-29 1990-12-18 Denis Jean Pierre Firearms ammunition, particularly game-shooting ammunition
US4964341A (en) * 1989-08-21 1990-10-23 Aai Corporation Projectile with ram air-extendible probe and ram air-extendible probe assembly therefor
US5677505A (en) * 1990-03-22 1997-10-14 Dittrich; William A. Reduced energy cartridge
US6492632B1 (en) * 1999-01-28 2002-12-10 Irvin Pollin Lock and slide mechanism for tube launched projectiles
US6415718B1 (en) * 1999-08-27 2002-07-09 Lambeth Properties Limited Training cartridge for a self loading gun
US6422149B1 (en) * 1999-08-27 2002-07-23 Lambath Properties Limited Blank training cartridge for a self loading gun
US6502516B1 (en) * 2000-01-18 2003-01-07 Anthony E. Kinchin Sabot shotgun slug assembly
US6679178B2 (en) * 2000-12-21 2004-01-20 Gueorgui M. Mihaylov Smooth bore barrel system with self spinning ammunition

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070227391A1 (en) * 2005-01-26 2007-10-04 De Aguiar Carlos F Q Non-lethal ammunition projectile
US7337725B2 (en) * 2005-01-26 2008-03-04 Condor S/A Industria Quimica Non-lethal ammunition projectile
USD852922S1 (en) 2017-09-14 2019-07-02 F. Richard Langner Slug for launching from a disruptor
USD853519S1 (en) 2017-09-14 2019-07-09 F. Richard Langner Piston for driving water out a disrupter

Also Published As

Publication number Publication date
ES2264033T3 (en) 2006-12-16
EP1543288A1 (en) 2005-06-22
DE50303386D1 (en) 2006-06-22
ATE326680T1 (en) 2006-06-15
AU2003266195A1 (en) 2004-04-19
EP1543288B1 (en) 2006-05-17
WO2004029539A1 (en) 2004-04-08
DE10244571C1 (en) 2003-12-04
US7331294B2 (en) 2008-02-19

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